DWG NO OD-2026-001
TITLE

From Sketch to Fairing: Modeling a Nose Cone

ISSUE
REV A
DATE 2026-04-30
SCALE NTS

A nose cone is the first thing the atmosphere sees and the last thing a CAD modeler gets right. It looks like a single curve and behaves like a committee: aerodynamics wants a Haack series, structures wants wall thickness, manufacturing wants a two-piece split, and the intern just wants the loft to stop twisting.

The good news is that the shape is genuinely mathematical. The Von Kármán ogive — the C=0 case of the Haack series — gives you a closed-form radius at every station along the axis. That means the profile is not a spline to be eyeballed; it is a table to be driven.

Drive the Curve, Don't Draw It

The amateur move is a three-point spline with tangency handles and hope. The professional move is a curve through computed stations: ten to twenty (x, r) pairs from the Haack equation, imported as a curve-through-points or rebuilt as an equation-driven spline. The result is smooth to second derivatives, which is what keeps both the pressure distribution and the zebra stripes honest.

STN 0.25L STN 0.40L STN 0.60L STN 0.80L L = 400.00 Ø164.00 VON KÁRMÁN OGIVE (HAACK C=0) r(x) = R/√π · √( θ − sin2θ/2 ), θ = arccos(1 − 2x/L) TIP R 0.8 MIN
FIG 3.1 — FAIRING PROFILE, STATIONED SCALE 1:4

Loft Discipline

A spline you can't write down is a shape you can't inspect.

Once the profile is an equation and the stations are a table, the fairing stops being a sculpture and becomes what every flight part must be: a number you can defend in a review board, at the machine shop, and at Mach 1.

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